US20060155508A1 - Spatial navigation system and method for programmable flying objects - Google Patents
Spatial navigation system and method for programmable flying objects Download PDFInfo
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- US20060155508A1 US20060155508A1 US11/033,219 US3321905A US2006155508A1 US 20060155508 A1 US20060155508 A1 US 20060155508A1 US 3321905 A US3321905 A US 3321905A US 2006155508 A1 US2006155508 A1 US 2006155508A1
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- ultrasonic
- distance
- moving object
- determining
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/18—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using ultrasonic, sonic, or infrasonic waves
- G01S5/26—Position of receiver fixed by co-ordinating a plurality of position lines defined by path-difference measurements
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/18—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using ultrasonic, sonic, or infrasonic waves
- G01S5/186—Determination of attitude
Definitions
- the present disclosure relates to flying toys.
- it relates to systems and methods for controlling the navigation of programmable flying toys.
- a significant contributor to the difficulty of operating toy aircraft is that the toy is not equipped with spatial positioning data.
- the toy receives command signals and blindly follows any command which at times results in disastrous crashes.
- current toys do not provide the user with the ability to preprogram flight sequences, paths, etc.
- a method of determining the position of a moving object in a space.
- a first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a ground station unit is determined.
- a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the ground station unit is determined.
- a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the ground station unit is determined.
- the first distance, the second distance and the third distance are utilized to determine the position of the moving object in relation to the ground station unit.
- the position of the moving object in relation to the ground station unit can be determined by using trilateration.
- the first distance can be determined by emitting an infrared light signal from the moving object to an infrared light receiver located at the ground station unit. Then, a time counter is initiated upon transmitting the infrared light signal. Next, a first ultrasonic signal is received from the first ultrasonic transmitter. The time counter is stopped upon receiving the first ultrasonic signal. Then, a predetermined speed constant is multiplied by a time indicated by the time counter.
- the second distance can be determined by emitting the infrared light signal from the moving object to the infrared light receiver located at the ground station unit. Then, the time counter is reinitiated upon transmitting the infrared light signal. Next, second ultrasonic signal is received from the second ultrasonic transmitter. The time counter is stopped upon receiving the second ultrasonic signal. Then, the predetermined speed constant is multiplied by the time indicated by the time counter.
- the second distance can be determined by reinitiating the time counter after a predetermined amount of time and then receiving a second ultrasonic signal from the second ultrasonic transmitter.
- the second ultrasonic signal can be sent after the predetermined amount of time passed since the first ultrasonic signal was received.
- the time counter is then stopped upon receiving the second ultrasonic signal at the ultrasonic receiver.
- the second distance will be product of the speed constant and the time counter.
- the third distance can be determined by emitting the infrared light signal from the moving object to the infrared light receiver located at the ground station unit. Then, the time counter is reinitiated upon transmitting the infrared light signal. Next, third ultrasonic signal is received from the third ultrasonic transmitter. The time counter is stopped upon receiving the third ultrasonic signal. Then, the predetermined speed constant is multiplied by the time indicated by the time counter.
- the third distance can be determined by reinitiating the time counter after a predetermined amount of time and then receiving a third ultrasonic signal from the third ultrasonic transmitter.
- the third ultrasonic signal can be sent after the predetermined amount of time elapsed since the second ultrasonic signal was received.
- the time counter is then stopped upon receiving the third ultrasonic signal at the ultrasonic receiver.
- the third distance will be product of the speed constant and the time counter.
- the first ultrasonic signal, the second ultrasonic signal, and the third ultrasonic signal have different ultrasonic frequencies from each other.
- Each ultrasonic signal may be received by one or more ultrasonic receivers.
- the moving object is configured to reach a specific destination by using the position of the moving object in relation to the specific destination.
- the moving object can also be configured to follow a specific path defined by a plurality of specific destinations.
- a space unit is mounted on the flying object.
- the space unit includes an ultrasonic receiver, an infrared light emitter and a microprocessor.
- the microprocessor can be configured to calculate a spatial position of the space unit based on a time differential between the time at which an infrared light is emitted by the infrared light emitter and the time at which ultrasonic signals are received by the ultrasonic receiver.
- the microprocessor can perform such calculation by using trilateration.
- a ground station unit has three ultrasonic transmitters, an infrared light receiver, and a base microprocessor. Each ultrasonic transmitter is distributed at each vertex of a predetermined equilateral triangle.
- the base microprocessor is configured to transmit an ultrasonic signal from each ultrasonic transmitter after detecting the infrared light emitted by the infrared light emitter.
- the flying object includes a motor control unit that controls a plurality of motors, the motor control unit coupled with the microprocessor.
- spatial navigation system also includes a second ultrasonic receiver and a remote control system using radio frequency modulation.
- the base microprocessor transmits an ultrasonic signal from each ultrasonic transmitter consecutively to the space unit.
- the base microprocessor can transmit an ultrasonic signal from each ultrasonic transmitter simultaneously.
- Each ultrasonic signal from each ultrasonic transmitter can have a different ultrasonic frequency form each other.
- there is a method of preventing crashes of a moving object against a surface A first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a surface (e.g. a wall or a floor) is determined. Then a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the surface is determined. Then it is determined a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the surface. The first distance, the second distance and the third distance are utilized to determine the position of the moving object in relation to the surface. Lastly, any movement of the flying object towards the surface prevented according to the position of the flying object.
- a surface e.g. a wall or a floor
- there is a method of determining the position of a moving object in a space by determining a first distance from a sonic receiver mounted on the moving object to a first sonic transmitter located at a ground station unit, determining a second distance from the sonic receiver mounted on the moving object to a second sonic transmitter located at the ground station unit, determining a third distance from the sonic receiver mounted on the moving object to a third sonic transmitter located at the ground station unit, and utilizing the first distance, the second distance and the third distance to determine the position of the moving object in relation to the ground station unit.
- there is method of determining the orientation of a moving object in a space first determines the position in space of a first point on the moving object. Then the position in space of a second point on the moving object is determined. Finally, the direction of movement is established to be parallel to a line defined by the first point and the second point.
- the position in space of the first point is established by determining a first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a ground station unit. Then a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the ground station unit is determined. Then it is determined a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the ground station unit. Lastly, the first distance, the second distance and the third distance are utilized to determine the first point in space in relation to the ground station unit. The position in space of the second point can be established in like manner.
- FIG. 1 illustrates a perspective view of a spatial navigation system for flying toys.
- FIG. 2A illustrates a perspective view of a space unit.
- FIG. 2B illustrates a block diagram of the components of the space unit depicted in FIG. 2A .
- FIG. 3A illustrates a perspective view of a ground station unit.
- FIG. 3B illustrates a block diagram of the components of the ground station unit depicted in FIG. 3A .
- FIG. 4 illustrates a flow chart for a method to determine the spatial position and orientation of the space unit.
- FIG. 5 illustrates a timing diagram of ultrasonic and infrared signals sent between the ground station unit and the space unit.
- FIG. 6A illustrates a perspective view of a remote control unit.
- FIG. 6B illustrates a block diagram of the components of the control unit depicted in FIG. 6A .
- FIG. 7 illustrates a flow chart for a method of navigation of the space unit.
- the method and system described below provide an improved way to navigate a flying toy as a helicopter, an airplane, a UFOs, etc.
- the flying toy is able to determine its position in a space by calculating the distance to three reference points on the ground.
- the flying toy uses three ultrasonic transmitters as the three reference points by timing an ultrasonic signal emitted from each of the ultrasonic transmitters to the flying toy.
- the ultrasonic signals used are acoustic waves with a frequency imperceptible by the human ear (i.e. higher than twenty thousand cycles per second or 20 KHz). As such, the ultrasonic signals are unnoticeable to the user. Further, sonic signals can also be used because they are equally functional although they will be noticeable by a user. Likewise, instead of infrared signals, which are invisible signals in the electromagnetic spectrum, other electromagnetic waves can be used such as radio or visible light signals.
- the method and system described below allow the flying toy to calculate its position and orientation in space permitting the toy to maneuver more intelligently. For instance, the flying toy can automatically fly within a limited region, be preprogrammed to follow flight sequences or navigation paths, or compensate for user errors avoiding crashes on the ground.
- FIG. 1 illustrates a perspective view of a spatial navigation system 100 for flying toys.
- the spatial navigation system 100 comprises a space unit 110 and a ground station unit 120 .
- the space unit 110 and the ground station unit 120 communicate with each other by using infrared 116 and ultrasonic signals 112 .
- the ground station unit 120 includes three ultrasonic transmitters 102 distributed away from each other forming a triangle.
- the ultrasonic transmitters 102 may be located equidistant from each other as to establish an equilateral triangle having a transmitter 102 at each vertex.
- the three ultrasonic transmitters 102 may be enclosed in the same housing as other components of the ground station unit 120 .
- the ultrasonic transmitters 102 may not be enclosed in the same housing yet they can be connected the rest of the ground station unit 120 via wired or wireless media.
- the ground station unit 120 also includes an infrared light receiver 104 .
- the infrared light receiver 104 can be positioned near the center of gravity of the triangle for better infrared reception.
- the space unit 110 comprises at least one infrared emitter 114 and at least one ultrasonic receiver 106 .
- the infrared emitter 114 can be a diode or an incandescent light emitting infrared light.
- the emitted infrared light 116 is then received by the infrared light receiver 104 in the ground station unit.
- the ultrasonic signals emitted by the ultrasonic transmitters 102 are received by the ultrasonic receiver 106 .
- FIG. 2A illustrates a perspective view of the space unit 110 .
- the space unit 110 can be a hovering flying vehicle having a carbon fiber supporting skeleton.
- the space unit 110 can have four propellers 210 each driven by a motor 220 .
- the motors 220 operate the propellers 210 necessary through suitable mechanical connections and gearing.
- Four lightweight outer rings 230 provide protection by absorbing any impact from crashing.
- the space unit 110 can have a plurality of propellers 210 propelled by a plurality of motors 220 which are encircled by a plurality of outer rings 230 .
- the space unit 110 can have two downward-facing ultrasonic receivers 106 separately mounted on bottom part of the space unit 110 .
- an infrared emitter diode 114 can be mounted on the bottom in order to emit infrared signals to the ground station unit 120 .
- FIG. 2B illustrates a block diagram of some of the components of the space unit 110 depicted in FIG. 2A .
- a microprocessor 250 is coupled to the ultrasonic receivers 106 , the infrared emitter 114 and a motor control unit 280 .
- the microprocessor 250 is pre-programmed with control software that calculates the movement of the space unit 110 by using the signals received by the ultrasonic receivers 106 and the infrared signal sent by the infrared emitter 114 .
- the calculated movement is transmitted from the microprocessor 250 to the motor control unit 280 which in turn operates the motors 220 and propellers 210 .
- the space unit 110 has gyro-stabilizing system 270 that controls the speed of each motor 220 to avoid malfunction such as flipping over.
- the microprocessor 250 can also be connected to a radio receiver 240 to receive radio command signals.
- FIG. 3A illustrates a perspective view of a ground station unit 120 .
- the ground station unit 120 is enclosed in one housing 300 which incorporates the three ultrasonic transmitters 102 , the infrared receiver 104 , a speaker 310 , light emitting diodes 320 and a microprocessor (not shown).
- the infrared receiver can be a phototransistor. In another embodiment, the infrared receiver can be a photoresistor.
- FIG. 3B illustrates a block diagram of the components of the ground station unit 120 including a microprocessor 350 .
- the infrared receiver 104 and the transmitters 102 are connected to the microprocessor 350 . Based on signals received by the infrared receiver 104 the microprocessor 350 controls the emission of ultrasonic signals through transmitters 102 .
- the microprocessor 350 is also coupled to the speaker 310 and the light emitting diodes 320 for indicating a status of the base station unit 120 and navigation of the space unit 110 .
- FIG. 4 illustrates a flow chart for a method 400 to determine the spatial position and orientation of the space unit 110 .
- the spatial position of space unit 110 in relation to the ground station unit 120 is calculated by determining the distance between each of the ultrasonic emitters 102 and the ultrasonic receiver 106 .
- the orientation of the space unit 110 in relation to the ground station unit 120 is calculated by using at least two ultrasonic receivers 106 and calculating their position in relation to the ground station unit 120 .
- the microprocessor 250 in the space unit 110 triggers an infrared light to be emitted from the light emitter 114 in the space unit 110 to the base station unit 120 .
- the infrared light may be emitted periodically. In another embodiment, the infrared light may be emitted every time the space unit 110 is turned on.
- the microprocessor 250 After sending the infrared signal, the microprocessor 250 starts a timer during process block 420 .
- the base station unit 120 captures the signal using the infrared light receiver 104 which then communicates to the microcontroller 350 that an infrared signal has been received.
- the microcontroller then commands a first ultrasonic transmitter 102 to emit an ultrasonic signal.
- the space unit 110 receives the first ultrasonic signal at the ultrasonic receiver 106 .
- the first ultrasonic signal is received by two ultrasonic receivers 106 for redundancy.
- the microprocessor 250 stops the timer and records the time delay during process block 440 . If a plurality of ultrasonic receivers 106 is used, the time elapsed between receiving the signal by one ultrasonic receiver 106 and the other can be slightly different. Therefore, the microcontroller 250 can calculate an average of the time delays for each ultrasonic receiver 106 .
- the orientation of the space unit 110 can also be calculated.
- the microcontroller 250 can be programmed with logic to perform geometrical and trigonometrical calculations to determine the orientation of the space unit 110 .
- the microcontroller 250 can establish the position of the straight line with respect to the ultrasonic transmitters 102 in the ground station unit 120 .
- the straight line defined by the ultrasonic receivers 106 is parallel to the direction in which the space unit moves when moving forward or backwards.
- the straight line defined by the ultrasonic receivers 106 is perpendicular to the direction in which the space unit moves when moving forward or backwards.
- the orientation of the space unit 110 can be determined by utilizing the distances from each of the ultrasonic transmitters 102 to each of the ultrasonic receivers 106 . If the system utilizes three ultrasonic transmitters 102 and two ultrasonic receivers 106 , a total of six distances can be used to determine the position of a line in space. The line in space defines the position and orientation of the space unit 110 .
- the microcontroller 250 calculates the distance from the first ultrasonic transmitter 102 to at least one ultrasonic receiver 106 . Because the ultrasonic signal moves at the speed of sound (i.e. 340 m/s), the distance can be determined by measuring the amount of time it takes for the signal to reach the ultrasonic receiver 106 . In other words, the distance is calculated by multiplying the time delay by the speed of sound.
- the base station unit 120 captures the signal using the infrared light receiver 104 which then communicates to the microcontroller 350 that an infrared signal has been received.
- the microcontroller then commands one of the ultrasonic transmitters 102 to emit an ultrasonic signal.
- the microprocessor 250 determines whether an ultrasonic signal has been sent from all three transmitters 102 . If the ultrasonic signal has not been sent to all three transmitters 102 , the microprocessor 250 in space unit 110 repeats the procedure. Namely, sends another infrared signal as described in process block 410 ; then, starts the timer again as described in process block 420 . Next, receives the ultrasonic signal at process block 430 , stops the timer and recording the time as in process block 440 , and calculates the distance from the ultrasonic transmitter 102 to the ultrasonic receiver 106 as in process block 450 .
- the microprocessor 350 at the ground station unit 120 may send the three ultrasonic signals consecutively without waiting for an infrared signal to initiate the process.
- the space unit 110 can be calibrated to automatically reset the timer three times, after a predetermined amount of time, such that the timer is reset every time a new ultrasonic signal is emitted by an ultrasonic transmitter 102 .
- the microprocessor 350 may send the three ultrasonic signals simultaneously.
- Each ultrasonic signal can have a different frequency thus providing a method of differentiating each arriving signal.
- Three timers can be used to record the travel time of each ultrasonic signal.
- the microprocessor 250 determines the orientation and position of the space unit 110 in process block 470 .
- the orientation of the space unit 110 is determined by using the position of two ultrasonic receivers 106 in relation to the ground station unit 120 .
- the spatial position of the space unit 110 is calculated by the microprocessor 250 using known three-dimensional trilateration methods that rely on the distances of three points in space in relation to an object. Since the flying speed of space unit 110 is relatively small (e.g. 1 m/s), it is assumed that the space unit 110 remains static during the time frame of three consecutive ultrasonic signal transmissions. Thus, the distances used in trilateration are assumed to be in relation to a static space unit 110 .
- FIG. 5 illustrates a timing diagram of ultrasonic and infrared signals sent between the ground station unit and the space unit.
- a first infrared signal 540 starts a timer at time 500 to count a first time delay 502 .
- the first infrared signal 540 triggers a first ultrasonic signal 550 . As soon as the first ultrasonic signal is received at time 504 the time delay 502 is recorded.
- a second infrared signal 541 starts a timer at time 506 to count a second time delay 508 .
- the second infrared signal triggers a second ultrasonic signal 560 . As soon as the second ultrasonic signal is received at time 510 the time delay 508 is recorded.
- a third infrared signal 542 starts a timer at time 512 to count a third time delay 514 .
- the third infrared signal triggers a third ultrasonic signal 570 . As soon as the third ultrasonic signal is received at time 516 the time delay 514 is recorded.
- FIG. 6A illustrates a perspective view of a remote control unit 600 .
- An antenna 610 transmits signals corresponding to user input received by control sticks 630 and navigation keys 620 .
- the navigation keys 620 and control sticks 630 permit the user to control yaw, roll and pitch motion, and throttle of the space unit 110 .
- the navigation keys can include auto-navigation keys which increase the freedom of the space unit 110 .
- FIG. 6B illustrates a block diagram of the components of the remote control unit 600 depicted in FIG. 6A .
- the control sticks 630 and the navigation keys 620 convey control signals to a microprocessor 650 .
- the microprocessor 650 in turn emits radio frequency signals to the space unit 110 through a radio transmitter 640 and antenna 610 .
- the remote control unit 600 can receive from the user a specific destination in space to which the space unit 110 must move.
- the microprocessor 650 can process the destination and transmit exact coordinates corresponding to the specific destination requested by the user.
- FIG. 7 illustrates a flow chart for a method of navigation 700 of the space unit 110 after a specific destination has been requested by the user.
- the space unit 110 determines its orientation information by utilizing the previously described method 400 which determines the spatial position and orientation of the space unit 110 .
- the space unit 110 is turned to point in direction of the specific destination.
- the space unit 110 moves forward one step.
- a step of the space unit 110 can be predefined to be movement of specific distance, or for a predetermined amount of time.
- Navigation of the space unit 110 can be achieved through the control of motors speed or rudder or elevators by the microprocessor in the space unit 110 .
- the microprocessor 250 in the control unit 110 determines whether the specific destination has been reached. If so, the destination is deemed complete in process block 750 . Otherwise, in process block 760 the space unit 110 determines once again its orientation information by utilizing the method 400 , which in turn determines the spatial position and orientation of the space unit 110 .
- decision block 770 the microprocessor 250 in the control unit 110 determines whether there has been a deviation from a straight path to the previously established specific destination. If so, method continues at process block 720 where the space unit 110 is turned to point in the ideal orientation towards the specific destination, moving forward one step at process block 730 , inquiring whether the destination has been reached at decision block 740 , and so on. Otherwise, if during decision block 770 the space unit 110 determines that there has not been a deviation, the method continues at process block 730 where the space unit 110 moves forward one step at process block 730 , inquires whether the destination has been reached at decision block 740 , and so on, until the final specific destination is reached.
- a spatial boundary can be preprogrammed in the space unit 110 such that the space unit 110 does not leave the coverage region of the ultrasonic transmitters 102 .
- the microprocessor 250 in the space unit 110 can be configured to operate the motor control unit so that the space unit 110 flies randomly within the coverage region.
- the microprocessor 250 in the space unit 110 can be preprogrammed with a plurality of destination points so as to define a path within the coverage region.
- a destination point for landing can be defined so that the space unit 110 can implement a series of take off, autopilot and landing functions.
- the microprocessor 250 can be programmed to compensate for user errors avoiding crashes on the ground. To that end, the microprocessor 250 may stop the space unit 110 to continue a downwards movement if the microprocessor calculates that the distance to any one of the ultrasonic transmitters 102 is less than a predetermined amount (e.g. 1 ft). On another embodiment, the microprocessor 250 may discontinue downwards movement of the space unit 110 if the microprocessor calculates its distance from the ground to be less than a predetermined amount.
- a predetermined amount e.g. 1 ft
- the moving object can be a flying toy, a bouncing toy, a rolling toy, etc.
- the disclosed system may be more beneficial for slow-moving objects
- the moving object can be any other flying object such as an airplane, helicopter, air balloon, missile, rocket, etc.
- the moving object can be any other mode of motorized and unmotorized transportation such as automobiles, trucks, boats, motorcycles, bicycles, tricycles, etc.
- the method and system can include more than three ultrasonic transmitters and more than one ultrasonic receiver.
- more than one moving object can be in communication and operation to the ground station.
- infrared radiation other type of electromagnetic radiation can be used.
- visible light waves, radio waves, microwaves, ultraviolet light waves, X-rays and gamma rays can also be utilized.
- sonic sound waves can be used instead of ultrasonic sound waves.
- sound waves of any frequency can be used regardless of whether they are audible or non-audible to the human ear.
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Abstract
Description
- 1. Field of the Disclosure
- The present disclosure relates to flying toys. In particular, it relates to systems and methods for controlling the navigation of programmable flying toys.
- 2. General Background
- Existing toy aircraft have generally been designed for remote control where the aircraft does not know its position or orientation in space. Rather, with a combination of propellers driven by a motor, an engine or the like, elevators and rudders, the toy aircraft flies only according to command signals received from a user during flight.
- These toy aircraft are generally difficult to operate because they require expertise to achieve a successful flight. Consequently, beginners can become frustrated because of disastrous results during the first time flights. Additionally, attempting to initiate a successful flight can be time-consuming which reduces the enjoyment of the activity.
- A significant contributor to the difficulty of operating toy aircraft is that the toy is not equipped with spatial positioning data. The toy receives command signals and blindly follows any command which at times results in disastrous crashes. Furthermore, current toys do not provide the user with the ability to preprogram flight sequences, paths, etc.
- In one aspect, there is a method of determining the position of a moving object (e.g. a flying toy) in a space. A first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a ground station unit is determined. Then a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the ground station unit is determined. Then it is determined a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the ground station unit. Lastly, the first distance, the second distance and the third distance are utilized to determine the position of the moving object in relation to the ground station unit. The position of the moving object in relation to the ground station unit can be determined by using trilateration.
- The first distance can be determined by emitting an infrared light signal from the moving object to an infrared light receiver located at the ground station unit. Then, a time counter is initiated upon transmitting the infrared light signal. Next, a first ultrasonic signal is received from the first ultrasonic transmitter. The time counter is stopped upon receiving the first ultrasonic signal. Then, a predetermined speed constant is multiplied by a time indicated by the time counter.
- The second distance can be determined by emitting the infrared light signal from the moving object to the infrared light receiver located at the ground station unit. Then, the time counter is reinitiated upon transmitting the infrared light signal. Next, second ultrasonic signal is received from the second ultrasonic transmitter. The time counter is stopped upon receiving the second ultrasonic signal. Then, the predetermined speed constant is multiplied by the time indicated by the time counter.
- In another aspect, the second distance can be determined by reinitiating the time counter after a predetermined amount of time and then receiving a second ultrasonic signal from the second ultrasonic transmitter. The second ultrasonic signal can be sent after the predetermined amount of time passed since the first ultrasonic signal was received. The time counter is then stopped upon receiving the second ultrasonic signal at the ultrasonic receiver. The second distance will be product of the speed constant and the time counter.
- The third distance can be determined by emitting the infrared light signal from the moving object to the infrared light receiver located at the ground station unit. Then, the time counter is reinitiated upon transmitting the infrared light signal. Next, third ultrasonic signal is received from the third ultrasonic transmitter. The time counter is stopped upon receiving the third ultrasonic signal. Then, the predetermined speed constant is multiplied by the time indicated by the time counter.
- In another aspect, the third distance can be determined by reinitiating the time counter after a predetermined amount of time and then receiving a third ultrasonic signal from the third ultrasonic transmitter. The third ultrasonic signal can be sent after the predetermined amount of time elapsed since the second ultrasonic signal was received. The time counter is then stopped upon receiving the third ultrasonic signal at the ultrasonic receiver. The third distance will be product of the speed constant and the time counter.
- In another aspect, the first ultrasonic signal, the second ultrasonic signal, and the third ultrasonic signal have different ultrasonic frequencies from each other. Each ultrasonic signal may be received by one or more ultrasonic receivers.
- In yet another aspect, the moving object is configured to reach a specific destination by using the position of the moving object in relation to the specific destination. The moving object can also be configured to follow a specific path defined by a plurality of specific destinations.
- In one aspect, there is a spatial navigation system to control a flying object (e.g. flying toy). A space unit is mounted on the flying object. The space unit includes an ultrasonic receiver, an infrared light emitter and a microprocessor. The microprocessor can be configured to calculate a spatial position of the space unit based on a time differential between the time at which an infrared light is emitted by the infrared light emitter and the time at which ultrasonic signals are received by the ultrasonic receiver. The microprocessor can perform such calculation by using trilateration. A ground station unit has three ultrasonic transmitters, an infrared light receiver, and a base microprocessor. Each ultrasonic transmitter is distributed at each vertex of a predetermined equilateral triangle. The base microprocessor is configured to transmit an ultrasonic signal from each ultrasonic transmitter after detecting the infrared light emitted by the infrared light emitter.
- In another aspect, the flying object includes a motor control unit that controls a plurality of motors, the motor control unit coupled with the microprocessor.
- In yet another aspect, spatial navigation system also includes a second ultrasonic receiver and a remote control system using radio frequency modulation.
- In another aspect, the base microprocessor transmits an ultrasonic signal from each ultrasonic transmitter consecutively to the space unit. Alternatively, the base microprocessor can transmit an ultrasonic signal from each ultrasonic transmitter simultaneously. Each ultrasonic signal from each ultrasonic transmitter can have a different ultrasonic frequency form each other.
- In one aspect, there is a method of preventing crashes of a moving object against a surface. A first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a surface (e.g. a wall or a floor) is determined. Then a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the surface is determined. Then it is determined a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the surface. The first distance, the second distance and the third distance are utilized to determine the position of the moving object in relation to the surface. Lastly, any movement of the flying object towards the surface prevented according to the position of the flying object.
- In another aspect, there is a method of determining the position of a moving object in a space by determining a first distance from a sonic receiver mounted on the moving object to a first sonic transmitter located at a ground station unit, determining a second distance from the sonic receiver mounted on the moving object to a second sonic transmitter located at the ground station unit, determining a third distance from the sonic receiver mounted on the moving object to a third sonic transmitter located at the ground station unit, and utilizing the first distance, the second distance and the third distance to determine the position of the moving object in relation to the ground station unit.
- In one aspect, there is method of determining the orientation of a moving object in a space. The method first determines the position in space of a first point on the moving object. Then the position in space of a second point on the moving object is determined. Finally, the direction of movement is established to be parallel to a line defined by the first point and the second point.
- The position in space of the first point is established by determining a first distance from an ultrasonic receiver mounted on the moving object to a first ultrasonic transmitter located at a ground station unit. Then a second distance from the ultrasonic receiver mounted on the moving object to a second ultrasonic transmitter located at the ground station unit is determined. Then it is determined a third distance from the ultrasonic receiver mounted on the moving object to a third ultrasonic transmitter located at the ground station unit. Lastly, the first distance, the second distance and the third distance are utilized to determine the first point in space in relation to the ground station unit. The position in space of the second point can be established in like manner.
- By way of example, reference will now be made to the accompanying drawings.
-
FIG. 1 illustrates a perspective view of a spatial navigation system for flying toys. -
FIG. 2A illustrates a perspective view of a space unit. -
FIG. 2B illustrates a block diagram of the components of the space unit depicted inFIG. 2A . -
FIG. 3A illustrates a perspective view of a ground station unit. -
FIG. 3B illustrates a block diagram of the components of the ground station unit depicted inFIG. 3A . -
FIG. 4 illustrates a flow chart for a method to determine the spatial position and orientation of the space unit. -
FIG. 5 illustrates a timing diagram of ultrasonic and infrared signals sent between the ground station unit and the space unit. -
FIG. 6A illustrates a perspective view of a remote control unit. -
FIG. 6B illustrates a block diagram of the components of the control unit depicted inFIG. 6A . -
FIG. 7 illustrates a flow chart for a method of navigation of the space unit. - The method and system described below provide an improved way to navigate a flying toy as a helicopter, an airplane, a UFOs, etc. The flying toy is able to determine its position in a space by calculating the distance to three reference points on the ground. The flying toy uses three ultrasonic transmitters as the three reference points by timing an ultrasonic signal emitted from each of the ultrasonic transmitters to the flying toy. The ultrasonic signals used are acoustic waves with a frequency imperceptible by the human ear (i.e. higher than twenty thousand cycles per second or 20 KHz). As such, the ultrasonic signals are unnoticeable to the user. Further, sonic signals can also be used because they are equally functional although they will be noticeable by a user. Likewise, instead of infrared signals, which are invisible signals in the electromagnetic spectrum, other electromagnetic waves can be used such as radio or visible light signals.
- Unlike previous navigation methods, the method and system described below allow the flying toy to calculate its position and orientation in space permitting the toy to maneuver more intelligently. For instance, the flying toy can automatically fly within a limited region, be preprogrammed to follow flight sequences or navigation paths, or compensate for user errors avoiding crashes on the ground. These and other features will be described below.
-
FIG. 1 illustrates a perspective view of aspatial navigation system 100 for flying toys. Thespatial navigation system 100 comprises aspace unit 110 and aground station unit 120. Thespace unit 110 and theground station unit 120 communicate with each other by using infrared 116 andultrasonic signals 112. For that purpose, theground station unit 120 includes threeultrasonic transmitters 102 distributed away from each other forming a triangle. In one approach, theultrasonic transmitters 102 may be located equidistant from each other as to establish an equilateral triangle having atransmitter 102 at each vertex. In some embodiments, the threeultrasonic transmitters 102 may be enclosed in the same housing as other components of theground station unit 120. In other embodiments, theultrasonic transmitters 102 may not be enclosed in the same housing yet they can be connected the rest of theground station unit 120 via wired or wireless media. Theground station unit 120 also includes aninfrared light receiver 104. In one embodiment, the infraredlight receiver 104 can be positioned near the center of gravity of the triangle for better infrared reception. - The
space unit 110, on the other hand, comprises at least oneinfrared emitter 114 and at least oneultrasonic receiver 106. Theinfrared emitter 114 can be a diode or an incandescent light emitting infrared light. The emittedinfrared light 116 is then received by the infraredlight receiver 104 in the ground station unit. In like manner, the ultrasonic signals emitted by theultrasonic transmitters 102 are received by theultrasonic receiver 106. -
FIG. 2A illustrates a perspective view of thespace unit 110. In one embodiment, thespace unit 110 can be a hovering flying vehicle having a carbon fiber supporting skeleton. Thespace unit 110 can have fourpropellers 210 each driven by amotor 220. Themotors 220 operate thepropellers 210 necessary through suitable mechanical connections and gearing. Four lightweightouter rings 230 provide protection by absorbing any impact from crashing. In other embodiments, thespace unit 110 can have a plurality ofpropellers 210 propelled by a plurality ofmotors 220 which are encircled by a plurality ofouter rings 230. - In one embodiment, the
space unit 110 can have two downward-facingultrasonic receivers 106 separately mounted on bottom part of thespace unit 110. Likewise, aninfrared emitter diode 114 can be mounted on the bottom in order to emit infrared signals to theground station unit 120. -
FIG. 2B illustrates a block diagram of some of the components of thespace unit 110 depicted inFIG. 2A . In particular, amicroprocessor 250 is coupled to theultrasonic receivers 106, theinfrared emitter 114 and amotor control unit 280. Themicroprocessor 250 is pre-programmed with control software that calculates the movement of thespace unit 110 by using the signals received by theultrasonic receivers 106 and the infrared signal sent by theinfrared emitter 114. The calculated movement is transmitted from themicroprocessor 250 to themotor control unit 280 which in turn operates themotors 220 andpropellers 210. - In one embodiment, the
space unit 110 has gyro-stabilizingsystem 270 that controls the speed of eachmotor 220 to avoid malfunction such as flipping over. Themicroprocessor 250 can also be connected to aradio receiver 240 to receive radio command signals. -
FIG. 3A illustrates a perspective view of aground station unit 120. In one embodiment, theground station unit 120 is enclosed in onehousing 300 which incorporates the threeultrasonic transmitters 102, theinfrared receiver 104, aspeaker 310,light emitting diodes 320 and a microprocessor (not shown). In one embodiment, the infrared receiver can be a phototransistor. In another embodiment, the infrared receiver can be a photoresistor. -
FIG. 3B illustrates a block diagram of the components of theground station unit 120 including amicroprocessor 350. Theinfrared receiver 104 and thetransmitters 102 are connected to themicroprocessor 350. Based on signals received by theinfrared receiver 104 themicroprocessor 350 controls the emission of ultrasonic signals throughtransmitters 102. Themicroprocessor 350 is also coupled to thespeaker 310 and thelight emitting diodes 320 for indicating a status of thebase station unit 120 and navigation of thespace unit 110. -
FIG. 4 illustrates a flow chart for amethod 400 to determine the spatial position and orientation of thespace unit 110. The spatial position ofspace unit 110 in relation to theground station unit 120 is calculated by determining the distance between each of theultrasonic emitters 102 and theultrasonic receiver 106. The orientation of thespace unit 110 in relation to theground station unit 120 is calculated by using at least twoultrasonic receivers 106 and calculating their position in relation to theground station unit 120. - During
process block 410, themicroprocessor 250 in thespace unit 110 triggers an infrared light to be emitted from thelight emitter 114 in thespace unit 110 to thebase station unit 120. In one embodiment, the infrared light may be emitted periodically. In another embodiment, the infrared light may be emitted every time thespace unit 110 is turned on. - After sending the infrared signal, the
microprocessor 250 starts a timer duringprocess block 420. Thebase station unit 120 captures the signal using the infraredlight receiver 104 which then communicates to themicrocontroller 350 that an infrared signal has been received. The microcontroller then commands a firstultrasonic transmitter 102 to emit an ultrasonic signal. - In
process block 430, thespace unit 110 receives the first ultrasonic signal at theultrasonic receiver 106. In another embodiment, the first ultrasonic signal is received by twoultrasonic receivers 106 for redundancy. - Once the microprocessor detects that the
ultrasonic receiver 106 has received an ultrasonic signal, themicroprocessor 250 stops the timer and records the time delay duringprocess block 440. If a plurality ofultrasonic receivers 106 is used, the time elapsed between receiving the signal by oneultrasonic receiver 106 and the other can be slightly different. Therefore, themicrocontroller 250 can calculate an average of the time delays for eachultrasonic receiver 106. - In another approach, if at least two
ultrasonic receivers 106 are used, the orientation of thespace unit 110 can also be calculated. Themicrocontroller 250 can be programmed with logic to perform geometrical and trigonometrical calculations to determine the orientation of thespace unit 110. By using the position of the twoultrasonic receivers 106 and the straight line joining the twoultrasonic receivers 106, themicrocontroller 250 can establish the position of the straight line with respect to theultrasonic transmitters 102 in theground station unit 120. In one embodiment, the straight line defined by theultrasonic receivers 106 is parallel to the direction in which the space unit moves when moving forward or backwards. In another embodiment, the straight line defined by theultrasonic receivers 106 is perpendicular to the direction in which the space unit moves when moving forward or backwards. - In yet another embodiment, the orientation of the
space unit 110 can be determined by utilizing the distances from each of theultrasonic transmitters 102 to each of theultrasonic receivers 106. If the system utilizes threeultrasonic transmitters 102 and twoultrasonic receivers 106, a total of six distances can be used to determine the position of a line in space. The line in space defines the position and orientation of thespace unit 110. - In
process block 450, themicrocontroller 250 calculates the distance from the firstultrasonic transmitter 102 to at least oneultrasonic receiver 106. Because the ultrasonic signal moves at the speed of sound (i.e. 340 m/s), the distance can be determined by measuring the amount of time it takes for the signal to reach theultrasonic receiver 106. In other words, the distance is calculated by multiplying the time delay by the speed of sound. - The
base station unit 120 captures the signal using the infraredlight receiver 104 which then communicates to themicrocontroller 350 that an infrared signal has been received. The microcontroller then commands one of theultrasonic transmitters 102 to emit an ultrasonic signal. - In
decision block 460, themicroprocessor 250 determines whether an ultrasonic signal has been sent from all threetransmitters 102. If the ultrasonic signal has not been sent to all threetransmitters 102, themicroprocessor 250 inspace unit 110 repeats the procedure. Namely, sends another infrared signal as described inprocess block 410; then, starts the timer again as described inprocess block 420. Next, receives the ultrasonic signal atprocess block 430, stops the timer and recording the time as inprocess block 440, and calculates the distance from theultrasonic transmitter 102 to theultrasonic receiver 106 as inprocess block 450. - In another embodiment, the
microprocessor 350 at theground station unit 120 may send the three ultrasonic signals consecutively without waiting for an infrared signal to initiate the process. Thespace unit 110 can be calibrated to automatically reset the timer three times, after a predetermined amount of time, such that the timer is reset every time a new ultrasonic signal is emitted by anultrasonic transmitter 102. - In yet another embodiment, the
microprocessor 350 may send the three ultrasonic signals simultaneously. Each ultrasonic signal can have a different frequency thus providing a method of differentiating each arriving signal. Three timers can be used to record the travel time of each ultrasonic signal. - After
decision block 460, if the alltransmitters 102 sent an ultrasonic signal, themicroprocessor 250 then determines the orientation and position of thespace unit 110 inprocess block 470. The orientation of thespace unit 110 is determined by using the position of twoultrasonic receivers 106 in relation to theground station unit 120. - The spatial position of the
space unit 110 is calculated by themicroprocessor 250 using known three-dimensional trilateration methods that rely on the distances of three points in space in relation to an object. Since the flying speed ofspace unit 110 is relatively small (e.g. 1 m/s), it is assumed that thespace unit 110 remains static during the time frame of three consecutive ultrasonic signal transmissions. Thus, the distances used in trilateration are assumed to be in relation to astatic space unit 110. -
FIG. 5 illustrates a timing diagram of ultrasonic and infrared signals sent between the ground station unit and the space unit. A firstinfrared signal 540 starts a timer attime 500 to count afirst time delay 502. The firstinfrared signal 540 triggers a firstultrasonic signal 550. As soon as the first ultrasonic signal is received attime 504 thetime delay 502 is recorded. - A second
infrared signal 541 starts a timer attime 506 to count asecond time delay 508. The second infrared signal triggers a secondultrasonic signal 560. As soon as the second ultrasonic signal is received attime 510 thetime delay 508 is recorded. - A third
infrared signal 542 starts a timer attime 512 to count athird time delay 514. The third infrared signal triggers a thirdultrasonic signal 570. As soon as the third ultrasonic signal is received attime 516 thetime delay 514 is recorded. -
FIG. 6A illustrates a perspective view of aremote control unit 600. Anantenna 610 transmits signals corresponding to user input received bycontrol sticks 630 andnavigation keys 620. Thenavigation keys 620 and control sticks 630 permit the user to control yaw, roll and pitch motion, and throttle of thespace unit 110. In one embodiment, the navigation keys can include auto-navigation keys which increase the freedom of thespace unit 110. -
FIG. 6B illustrates a block diagram of the components of theremote control unit 600 depicted inFIG. 6A . The control sticks 630 and thenavigation keys 620 convey control signals to amicroprocessor 650. Themicroprocessor 650 in turn emits radio frequency signals to thespace unit 110 through aradio transmitter 640 andantenna 610. - In one embodiment, the
remote control unit 600 can receive from the user a specific destination in space to which thespace unit 110 must move. Themicroprocessor 650 can process the destination and transmit exact coordinates corresponding to the specific destination requested by the user. -
FIG. 7 illustrates a flow chart for a method ofnavigation 700 of thespace unit 110 after a specific destination has been requested by the user. Inprocess block 710, thespace unit 110 determines its orientation information by utilizing the previously describedmethod 400 which determines the spatial position and orientation of thespace unit 110. - During
process block 720, thespace unit 110 is turned to point in direction of the specific destination. Inprocess block 730, thespace unit 110 moves forward one step. A step of thespace unit 110 can be predefined to be movement of specific distance, or for a predetermined amount of time. Navigation of thespace unit 110 can be achieved through the control of motors speed or rudder or elevators by the microprocessor in thespace unit 110. - In
decision block 740, themicroprocessor 250 in thecontrol unit 110 determines whether the specific destination has been reached. If so, the destination is deemed complete inprocess block 750. Otherwise, in process block 760 thespace unit 110 determines once again its orientation information by utilizing themethod 400, which in turn determines the spatial position and orientation of thespace unit 110. - Subsequently, in
decision block 770, themicroprocessor 250 in thecontrol unit 110 determines whether there has been a deviation from a straight path to the previously established specific destination. If so, method continues at process block 720 where thespace unit 110 is turned to point in the ideal orientation towards the specific destination, moving forward one step atprocess block 730, inquiring whether the destination has been reached atdecision block 740, and so on. Otherwise, if duringdecision block 770 thespace unit 110 determines that there has not been a deviation, the method continues at process block 730 where thespace unit 110 moves forward one step atprocess block 730, inquires whether the destination has been reached atdecision block 740, and so on, until the final specific destination is reached. - In another embodiment, a spatial boundary can be preprogrammed in the
space unit 110 such that thespace unit 110 does not leave the coverage region of theultrasonic transmitters 102. Themicroprocessor 250 in thespace unit 110 can be configured to operate the motor control unit so that thespace unit 110 flies randomly within the coverage region. In another approach, themicroprocessor 250 in thespace unit 110 can be preprogrammed with a plurality of destination points so as to define a path within the coverage region. In yet another embodiment, a destination point for landing can be defined so that thespace unit 110 can implement a series of take off, autopilot and landing functions. - In another embodiment, the
microprocessor 250 can be programmed to compensate for user errors avoiding crashes on the ground. To that end, themicroprocessor 250 may stop thespace unit 110 to continue a downwards movement if the microprocessor calculates that the distance to any one of theultrasonic transmitters 102 is less than a predetermined amount (e.g. 1 ft). On another embodiment, themicroprocessor 250 may discontinue downwards movement of thespace unit 110 if the microprocessor calculates its distance from the ground to be less than a predetermined amount. - There are other variations of the system and method disclosed herein. For example, the moving object can be a flying toy, a bouncing toy, a rolling toy, etc. Although the disclosed system may be more beneficial for slow-moving objects, the moving object can be any other flying object such as an airplane, helicopter, air balloon, missile, rocket, etc. In addition, the moving object can be any other mode of motorized and unmotorized transportation such as automobiles, trucks, boats, motorcycles, bicycles, tricycles, etc.
- The method and system can include more than three ultrasonic transmitters and more than one ultrasonic receiver. In addition, more than one moving object can be in communication and operation to the ground station.
- Furthermore, besides infrared radiation, other type of electromagnetic radiation can be used. For example, visible light waves, radio waves, microwaves, ultraviolet light waves, X-rays and gamma rays can also be utilized. In like manner, sonic sound waves can be used instead of ultrasonic sound waves. In other words, sound waves of any frequency can be used regardless of whether they are audible or non-audible to the human ear.
- Although certain illustrative embodiments and methods have been disclosed herein, it will be apparent form the foregoing disclosure to those skilled in the art that variations and modifications of such embodiments and methods may be made without departing from the true spirit and scope of the art disclosed. Many other examples of the art disclosed exist, each differing from others in matters of detail only. Accordingly, it is intended that the art disclosed shall be limited only to the extent required by the appended claims and the rules and principles of applicable law.
Claims (33)
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